| 飞翼飞机稳定性与操纵性研究 |
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| 引用本文： | 马松辉,吴成富,陈怀民.飞翼飞机稳定性与操纵性研究[J].飞行力学,2006,24(3):17-21. |
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| 作者姓名： | 马松辉 吴成富 陈怀民 |
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| 作者单位： | 西北工业大学,无人机特种技术国防科技重点实验室,陕西,西安,710072 |
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| 摘 要： | 以某飞翼飞机为例,讨论了典型飞翼飞机的基本操稳特性和动态特性。并对飞翼布局飞机和常规布局飞机的主要气动导数作了对比研究,简要说明了二者在操稳特性上的不同之处及其产生的原因,为控制增稳系统的设计提供了依据。
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| 关 键 词： | 飞翼 无尾飞机 操稳特性 |
| 文章编号： | 1002-0853(2006)03-0017-05 |
| 收稿时间： | 2005-08-20 |
| 修稿时间： | 2006-06-12 |
Study on Stability and Manoeuvrability of Flying Wing Aircraft |
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| MA Song-hui,WU Cheng-fu,CHEN Huai-min.Study on Stability and Manoeuvrability of Flying Wing Aircraft[J].Flight Dynamics,2006,24(3):17-21. |
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| Authors: | MA Song-hui WU Cheng-fu CHEN Huai-min |
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| Abstract: | A flying wing aircraft has many very different characteristics on stability and manoeuvrability compared to a traditional aircraft.This paper takes the flying wing aircraft FWX1 as an example to explain the stability and manoeuvrability of a flying wing aircraft,which is the base for control and stability augmentation system design. |
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| Keywords: | flying wing tailless aircraft stability and manoeuvrability |
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